Limitations Flashcards

1
Q

Flight Maneuvering Load Factor Limits

A

-1 to +2.5 in Clean config
O to +2 in other configs

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2
Q

Runway altitude
Runway Slope
Runway width (nominal and minimal)

A

9200 ft
+/- 2%
45m, min 30 meter

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3
Q

Crosswind

Tailwind

Cargo door
Passenger door

A

35 kt takeoff (38 CEO)
38 kt landing

15 kt tail land/take off. (Full flaps if tail > 10 kt)

Operations 40kt (50 if nose into wind) closed before 65 kt.
Operations 65kr

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4
Q

MAXIMUM RECOMMENDED CROSSWIND ON WET AND CONTAMINATED RUNWAYS

A

Brake Action - Wind
5 - 35
4 - 29
3 - 25
2 - 20
1 - 15

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5
Q

Max Windows Open speed

A

200kt

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6
Q

VMO/MMO and Max Flaps speed

A

VMO - 350
MMO - M 0.82
1 - 230
1+f - 215
2 - 200
3 - 185
Full - 177

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7
Q

Maximum speed GEAR
VLE
VLO Ex
VLO Re

A

VLE - 280
VLO Ex - 250
VLO Re - 220

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8
Q

Max Tire speed

A

195 kt

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9
Q

Max Wipers speed

A

230 kt

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10
Q

Weight Limitations NEO
Taxi
Takeoff
Landing
Zero Fuel

A

77 400
77 000
67 400
64 300

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11
Q

Weight Limitations CEO
Taxi
Takeoff
Landing
Zero Fuel

A

73 900
73 500
64 500
61 000

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12
Q

Avionics Ventilation max temp for no limitation

A

49 C

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13
Q

Max Differential Cabin Pressure

A

9 PSI
-1 PIS
Safety relief Valve 8.6 PSI

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14
Q

Autopilot Function
At takeoff
In Approach Precision
In Approach Non-Precision

A

100 ft AGL or after 5 sec
200 ft AGL
250 ft AGL

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15
Q

Minimum Decision Height
Cat ll
Cat lll Fail Passive (Single)
Cat lll Fail Operational (Dual)

A

100 ft
50 ft
Alert Height 100 ft. 75m vis

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16
Q

Maximum wind for CAT II and III

A

Head 30
Cross 20 (15 for automatic rollout with OEI)
Tail 10

18
Q

Glide slope for Automatic Landings

A

-2.5° to -3.25°

19
Q

APU Limitations
Attempts (Wait time)
Operational Envelope
Assisted Engine start
For anti-ice

A

3 Attempts (Wait 60 min)
Bleed Air up to 22 500 ft (Single Pack) 15 000ft (Dual pack) , Elec full envelope
20 000 ft
Not permitted

20
Q

TOGA Time limits

A

All engines 5 min
OEI 10 min

21
Q

Oil Temperature NEO
Max Continuous
Min start
Min before takeoff

A

140°
-40°
19°

22
Q

Oil Temperature CEO
Max Continuous
Min start
Before Idle is Exceeded
Min before takeoff

A

155°
-40°
-10°
50°

23
Q

Minimum Oil Quantity CEO and NEO

A

NEO
- 10.6 qt, or
- 8.9 qt + estimated consumption.
Maximum estimated consumption = 0.45 qt/h.

CEO
11 qt + estimated consumption
Average estimated consumption = 0.3 qt/h.

24
Q

Starter Limit NEO and CEO

A

NEO
Cycle = 3 attempts
Each Cycle => wait 60s
3 Cycles => wait 15min
CEO
Cycle = 1 attempt
Each Cycle => 15s
3 Cycles => 60 min of 5 min of cont crank

25
Q

Engine start max crosswind (CEO NEO)

A

NEO 45kt
CEO 35 kt

26
Q

Max altitude for Flaps extended

27
Q

JET A1 Fuel Temperature

A

-43° C (Jet A -36)
55° C

28
Q

MAX Fuel Imbalance
Heavier tank - Mas Asymmetry

A

Takeoff
FULL - 500kg
3000kg - 1050kg
1450kg - 1450kg
(Outer 370kg)

Landing
Full - 1500kg
4300kg - 1600kg
2250kg - 2250kg

Outer Max 690kg

29
Q

Minimum Fuel for takeoff

30
Q

Definition of Icing Conditions

A

OAT <= 10°C
Visible Moisture (Clouds, fog with less than 1 sm (1600m) vis or less, rain, snow, sleet or ice crystals) Also when taxiways and runways have snow, slush or water that might be ingested into engines

31
Q

Definition of severe ice accretion

A

Ice accumulation on airframe reaches 5 mm or more

32
Q

Max brake Temp (Fan off)

33
Q

Taxi speeds with Damages tires

A

One tire 7kr
two tires (on same gear) 3kt
Max angle 30°